A shrink mechanism (300) for use with a landing gear (200A) of an aircraft (100) is provided. The landing gear includes an outer sleeve (310) at least partially surrounding a shock strut (210), the shrink mechanism has a shaft (312) rotatably coupled to the outer sleeve about a shaft rotation axis (314), the shaft being disposed perpendicular to a centerline (316, 316') of the shock strut, an anchor arm (318) coupled to the shaft, the anchor arm being configured to couple to a structure (320) within a wing (322) of the aircraft, a shrink arm (324) coupled to the shaft, the shrink arm and the anchor arm being coupled to the shaft so as to rotate as a unit with the shaft about the shaft rotation axis, and a shrink link (326) rotatably coupled to the shrink arm, the shrink link being configured to rotatably couple to the shock strut.


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    Titel :

    Tren de aterrizaje retráctil semipalancado


    Beteiligte:
    DAHL BRUCE A (Autor:in) / SAKURAI SEIYA (Autor:in)

    Erscheinungsdatum :

    2024-06-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Spanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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